Integrated remote control Land air amphibious drone equipped with a large capacity battery and efficient motor

Short Description:

Overall Performance ParametersModel structure: 4-axisPower source: Lithium battery (soft pack battery)Diagonal wheelbase: 1000mmBody Material: Carbon FiberDrone deployment time: ≤ 2minPositioning and Navigation: RTK+GPSControl radius of data communication link: ≥ 15kmTransmission distanc...


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Overall Performance Parameters

  1. Model structure: 4-axis
  2. Power source: Lithium battery (soft pack battery)
  3. Diagonal wheelbase: 1000mm
  4. Body Material: Carbon Fiber
  5. Drone deployment time: ≤ 2min
  6. Positioning and Navigation: RTK+GPS
  7. Control radius of data communication link: ≥ 15km
  8. Transmission distance of image and video links: ≥ 15km
  9. Maximum takeoff weight: 18kg
  10. Maximum load: 2kg
  11. Maximum load flight time: 10-15min
  12. Maximum flight speed: ≥ 20m/s
  13. Maximum climb speed: ≥ 6m/s
  14. Maximum descent speed: ≥3 m/s
  15. ★Maximum speed on land: 2m/s
  16. Maximum land climbing: 25%
  17. Maximum wind resistance: ≥ Level 5 (Instantaneous Level 6)
  18. Cruise altitude for homework: 20-1000 meters
  19. Camera: Front facing high-definition camera
  20. Obstacle avoidance radar: front and rear obstacle avoidance distance of 1-20 meters
  21. Battery: 1 set of 22000mah
  22. Protection level: IP45
  23. Working temperature: -20 ºC to 50 ºC

24.Land and Air Amphibious: ★ Structural Form: Designed with a land and air amphibious structure, the bottom of the fuselage is equipped with 4 walking wheels, which can be remotely controlled for land travel; Drone land travel speed: ≥ 2m/s. Remote control: The drone remote control and land travel remote control use one remote control. The parameters need to be consistent with the testing report issued by a third-party testing agency with qualifications for rotor unmanned aerial vehicle inspection, and the cover of the testing report should have CMA and CNAS marks. This ★ parameter needs to be consistent with the testing report issued by a third-party testing agency with qualifications for rotor unmanned aerial vehicle inspection. The cover of the testing report should have CMA and CNAS logos, and the testing report should be stamped with the product manufacturer’s official seal (fresh seal) as proof; At the same time, provide the authorization certificate and authorization scope details issued by the market supervision department to third-party testing


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